[IGSREPORT-28884] Wk 2223 IGLOS Final Orbits
acc
acc at igs.org
Sat Sep 3 01:28:12 UTC 2022
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2223 (Aug 14, 2022 - Aug 20, 2022)
Contact: acc at igs.org
COMBINATION STRATEGY:
---------------------
Ephemeris are combined as weighted averages computed over all centres.
Each centre and satellite is given a position weight computed from the
center's absolute deviation to the unweighted average orbit after removing
small differences in the reference frames. These weights were applied in a
second iteration to estimate Helmert transformation parameters for each
center. Finally the transformation parameters with respect to the combined
solution and the RMS of the fit are reported in Tables 2.2223.
For long arc computations the Earth Orientation Parameters (EOPs) are fixed
to the values of the final IGS (GPS) combination.
SOFTWARE:
---------
The weighted average software used was originally developed by T. Springer
and G. Beutler in 1993. The GPS long arc orbit analysis software used here for
individual centre ephemeris evaluation was developed by Beutler et al. at the
Astronomical Institute of the University of Bern (AIUB). For more details on
the orbit combination and complete references for both software see:
Beutler G., Kouba J. and T. Springer, 1995, Combining the orbits of the IGS
Analysis Centers, Bulletin Geodesique, 69, pp 200-222.
Kouba J., Mireault Y. and F. Lahaye, 1995, 1994 IGS Orbit/Clock Combination
and Evaluation, Appendix I of the Analysis Coordinator Report, International
GPS Service for Geodynamics (IGS) 1994 Annual Report, pp. 70-94.
Kouba J. and Y. Mireault, 1996, IGS Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1995 Annual Report,
pp. 45-76.
Kouba J. and Y. Mireault, 1997, Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1996 Annual Report,
pp. 55-100.
Weber R., 2000, IGS Technical Report 1999
PRODUCTS GENERATED:
-------------------
The combined IGL-ephemerides are written to daily files in the SP3-format.
The satellite accuracy codes in the header are based on the weighted rms.
for each satellite. Note, that the result files contain all satellites
that were analysed by at least one center. We refer to the 'REMARKS' section
below, in case a satellite or center was excluded from the combination.
The following naming convention is used for the result files:
igl2223[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2223 in the SP3 format.
igl22237.sum Combination Report for GPS Week 2223.
REMARKS concerning the IGL Orbit Combination:
---------------------------------------------
Starting 16-Sep-2012 (GPS Week 1706, day 0, MJD 56186) the CODE Analysis Center
began submitting two solutions: COD (3d SNX with 3d orbital arcs) and COF (1d
SNX with 1d orbital arcs). The COF clocks and orbits are included for
comparison only; the COD solution is included with weight.
1. Broadcast (brd) orbits and clocks are included in the combination for
statistics only.
2. Having only a few satellites the mcc orbits are included in the combination
for statistics only. The grg orbits are introduced for the first time
starting 02-Jan-2011 (GPS Week 1617) but only for statistics until
22-May-2011 (GPS Week 1637). The bkg orbits were no longer included after
21-May 2011 (GPS Week 1636). The emx orbits are introduced with full weight
for the first time starting 11-Sep-2011 (GPS Week 1653).
3. From 01-May-2005 (GPS Week 1321; MJD 53491) [IGSMAIL-5151] until 4-Nov-2006
BKG, ESA, and CODE referred their GLONASS orbit products to the following
satellite antenna offset (SAO) values (expressed in the spacecraft body
frame):
X/Y/Z = 0.000/0.000/0.000 meter for GLONASS and
X/Y/Z = -0.545/0.000/0.000 meter for GLONASS-M SVs.
Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011
(GPS Week 1631, day 6, MJD 55667) the absolute antenna model is introduced
(IGSMAIL #5438). The antenna phase center offsets and phase center variations
are given in the file:
https://files.igs.org/pub/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
https://files.igs.org/pub/station/general/igs08.atx
Starting 29-Jan-2017 (GPS Week 1934, day 0, MJD 57782) the absolute antenna
model file has been updated to igs14.atx to be consistent with IGS14.
See IGSMAIL #7399 for more information
https://files.igs.org/pub/station/general/igs14.atx
4. The satellite clock values in the combined orbit files are taken from the
broadcast files. The following gps/glonass time offsets were added to the
broadcast clocks. Before GPS Week 1637, the time offsets were derived
from the bkg summary files; starting Week 1637 the offsets are derived
from the gfz summary files.
Day | applied clock offset
----+---------------------
0 | -6.4 ns
1 | -0.5 ns
2 | -7.3 ns
3 | -0.4 ns
4 | -5.4 ns
5 | -7.4 ns
6 | -7.0 ns
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Table 1 summarizes all statistics for the week. It contains means and standard
deviations over the week of satellite ephemeris and clock correction
transformation parameters for each centre (Tables 1.2223, 1a.2223).
Table 2 contains the complete ephemeris and clock correction transformation
parameters (includes both the apriori and a posteriori values) for each
centre and each day (Tables 2.2223.0-6)
Table 3 contains two types of daily RMS for each satellite and centre, along
with the computed satellite position sigmas for the combined orbits
(tables 3.2223.0-6).
The first type of satellite RMS is based on orbit combination and the
second RMS type is a result of the 7-day arc evaluation of each centre
ephemerides.
Table 1: Week 2223 summary. (Aug 14, 2022 - Aug 20, 2022)
Table 1.2223.a GPS week : 2223 MJD: 59805.0-59811.0
Mean and standard deviations of transformation parameters to the
combined IGL orbit.
WRMS - orbit RMS weighted by the SP3 header accuracy codes.
STA - Mean number of stations in the daily solutions.
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 0 -2 -12 -22 -1 .16 25 21 | 26639 -1378 2959 8238
| 0 1 2 9 11 32 .04 | 3523 2084
emx n/a| -2 1 15 30 -15 17 -.05 42 34 | -8486 -1094 2978 8225
| 2 1 3 33 22 55 .05 | 8782 1724
esx n/a| 0 1 3 -1 28 16 -.13 28 21 | -2012 -700 2956 11087
| 1 1 2 28 21 41 .05 | 13205 1952
gfz n/a| 0 0 -2 -3 10 12 -.06 27 17 | 0 -960 3001 8075
| 0 1 2 18 24 31 .05 | 0 1805
grg n/a| 4 -1 -9 -24 39 -13 .39 26 20 | -4510 -1129 2954 7725
| 1 1 5 16 27 40 .06 | 3166 1827
iac n/a| 0 0 3 12 -43 -17 -.26 23 21 | -1876 -557 3017 9815
| 0 1 4 24 44 75 .06 | 2755 764
Table 1.2223.b GPS week : 2223 MJD: 59805.0-59811.0
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
R01 | 23 22 20 21 20 19 20 |
R02 | 6 8 8 9 9 10 10 |
R03 | 9 11 9 10 8 9 9 |
R04 | 12 13 9 11 10 8 11 |
R05 | 9 10 11 11 10 8 9 |
R07 | 10 10 10 9 9 8 7 |
R08 | 12 12 10 9 8 8 7 |
R09 | 11 9 7 11 8 7 8 |
R11 | 7 6 7 8 9 10 12 |
R12 | 7 7 7 8 9 9 9 |
R13 | 19 15 12 15 15 11 12 |
R14 | 7 5 7 7 6 7 7 |
R15 | 10 7 6 6 8 7 6 |
R17 | 8 8 9 8 8 8 8 |
R18 | 9 11 9 9 9 11 8 |
R19 | 22 20 18 27 25 24 26 |
R20 | 22 25 23 25 20 24 25 |
R21 | 8 9 10 10 8 8 8 |
R24 | 9 9 12 11 10 9 9 |
R25 | 0 0 0 0 0 0 0 |
Table 1.2223.c GPS week : 2223 MJD: 59805.0-59811.0
Daily transformation of broadcast orbits (brd) to the combined IGL orbit.
Mean and standard deviations of the transformation parameters for the
whole gpsweek.
CEN WEEK DAY | DX DY DZ RX RY RZ SCL RMS WRMS | TOFT TDRFT
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm] | [ps] [ps/d]
-------------+------------------------------------------------------------+----------------
brd 2223 0 | -40 78 127 -1568 -534 11780 83.4 1475 1475 | -6408 0
brd 2223 1 | -112 63 223 -982 -1242 6307 82.8 1518 1518 | -544 0
brd 2223 2 | 20 -41 137 -1409 51 12070 81.1 1459 1459 | -7299 0
brd 2223 3 | -19 86 147 -827 -1648 6507 78.0 1449 1449 | -424 0
brd 2223 4 | 33 -75 200 1916 141 -8998 78.3 1395 1395 | -5419 0
brd 2223 5 | 22 -25 53 756 -1560 1123 80.9 1618 1618 | -7442 0
brd 2223 6 | 70 17 -15 502 -1116 2376 81.0 1848 1848 | -6952 0
-------------+------------------------------------------------------------+----------------
brd 2223 mean| -3 14 124 -230 -844 4452 80.8 1537 1537 | -4926 0
brd 2223 sdev| 60 64 82 1305 737 7253 2.0 153 153 | 3108 0
Table 2: Daily transformation of each centre to the combined IGL orbit and
clocks for each day of the week. The transformation displayed is the
sum of a priori and estimated transformations.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.2223.0 GPS week: 2223 Day: 0 MJD: 59805
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -2 0 -2 -19 -32 -39 .13 22 20 | 27081 -76 3014 8119
emx n/a| 0 1 9 -29 -20 14 -.09 45 37 | -1254 -179 2993 8114
esx n/a| 1 0 1 53 26 17 -.07 28 21 | -25041 1087 2995 10236
gfz n/a| 0 0 -1 -16 15 25 -.07 21 14 | 0 808 3056 7588
grg n/a| 3 0 -3 3 -8 -78 .35 28 21 | -6619 66 3025 7701
iac n/a| 0 -1 3 35 6 83 -.32 34 31 | -2926 -462 3049 9789
Table 2.2223.1 GPS week: 2223 Day: 1 MJD: 59806
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 -1 1 -26 -13 -1 .18 23 19 | 32903 -2007 2889 7865
emx n/a| -6 0 15 21 -33 36 -.04 41 34 | 2267 -834 2908 7796
esx n/a| -1 0 0 -38 25 2 -.10 27 20 | 13289 -1698 2876 11431
gfz n/a| 0 0 0 27 34 22 -.15 25 16 | 0 -1401 2930 7537
grg n/a| 2 -1 -17 -15 51 -5 .30 28 23 | 197 -1637 2859 7381
iac n/a| 0 0 6 46 -56 -88 -.26 28 25 | 2259 607 2944 9833
Table 2.2223.2 GPS week: 2223 Day: 2 MJD: 59807
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 -2 -1 -7 -7 6 .15 24 23 | 23945 -2629 2766 7497
emx n/a| -2 1 18 62 20 28 -.10 43 35 | -16423 -1438 2820 7545
esx n/a| -3 2 6 -1 54 44 -.15 28 20 | -12432 -1571 2788 11092
gfz n/a| 0 0 0 -8 38 23 -.09 25 17 | 0 -2218 2786 7619
grg n/a| 4 -2 -17 -32 40 -42 .39 20 17 | -6224 -2390 2751 6831
iac n/a| -1 0 7 15 -110 -36 -.33 21 20 | -4044 -1098 2856 9614
Table 2.2223.3 GPS week: 2223 Day: 3 MJD: 59808
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 -1 -6 -13 -14 -48 .22 28 20 | 29783 -1794 2777 8514
emx n/a| -2 2 13 28 -16 1 -.07 41 32 | -110 -355 2789 8597
esx n/a| -1 1 3 -8 39 69 -.09 26 20 | -727 -1676 2762 10978
gfz n/a| 0 2 -4 -21 7 50 -.01 32 20 | 0 -1138 2831 8260
grg n/a| 4 -3 -9 -19 21 18 .47 31 22 | 12 -1006 2769 8015
iac n/a| -1 0 5 -7 -52 -70 -.28 22 20 | 1974 -295 2765 9242
Table 2.2223.4 GPS week: 2223 Day: 4 MJD: 59809
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 0 -3 -12 -40 36 .21 29 29 | 23732 2774 2999 9054
emx n/a| 0 2 15 37 9 -71 .05 41 34 | -9231 1586 3030 9057
esx n/a| 0 2 5 -14 -15 -53 -.15 28 22 | -3539 2979 3001 11049
gfz n/a| 0 0 -2 0 -23 -39 -.02 28 19 | 0 2198 3061 8963
grg n/a| 4 -2 -11 -33 34 41 .44 25 22 | -6771 2336 2993 8424
iac n/a| 0 0 4 4 10 43 -.26 17 17 | -3073 75 3007 9629
Table 2.2223.5 GPS week: 2223 Day: 5 MJD: 59810
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -3 1 -1 -13 -25 4 .10 28 20 | 24984 -3018 3143 8227
emx n/a| -3 1 18 72 -36 -4 -.00 40 32 | -18884 -3369 3166 8181
esx n/a| 0 0 4 -13 34 -13 -.22 27 19 | 6779 -2033 3144 11238
gfz n/a| 0 -2 -4 -17 -20 -20 -.01 31 18 | 0 -2462 3164 8014
grg n/a| 6 0 -4 -50 51 -33 .41 22 18 | -6279 -2950 3151 7598
iac n/a| -1 -1 -2 16 -18 48 -.21 18 17 | -3691 -1563 3295 10084
Table 2.2223.6 GPS week: 2223 Day: 6 MJD: 59811
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 0 -2 4 -19 33 .14 24 17 | 24045 -2901 3128 8394
emx n/a| -2 0 19 24 -33 114 -.08 44 34 | -15772 -3072 3143 8287
esx n/a| -2 0 4 9 34 44 -.13 29 23 | 7583 -1993 3131 11589
gfz n/a| 0 0 -5 13 19 27 -.07 30 14 | 0 -2511 3182 8546
grg n/a| 5 -1 -5 -22 81 8 .38 26 22 | -5892 -2326 3133 8130
iac n/a| 0 3 -1 -24 -79 -105 -.15 21 20 | -3637 -1167 3208 10518
Table 3: Daily fit for each satellite and each centre resulting from weighted
average combination and from long arc orbit dynamics (7-day). The
first IGL column gives resulting satellite accuracy measures found in
SP3 header. The last IGL column gives the RMS fit of the IGL orbit
when processed through the 7-day arc evaluation.
"E" stands for eclipsing satellites (earth).
"M" stands for eclipsing satellites (moon).
"X" stands for excluded from the statistics but included in IGL orbit.
"T" stands for Total long arc orbit RMS for all satellites.
"NE" stands for long arc orbit RMS for Non-Eclipsing satellites only.
"MEDI" stands for median of the centre's satellite RMS.
"MD"
Units: mm.
Table 3.2223.0 GPS week: 2223 Day: 0 MJD: 59805
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 827 46 66 62 38 50 41 22 | 93 42 64 82 74 51 60
R02E | 2446 9 29 12 10 13 12 6 | 111 101 111 114 115 113 110
R03E | 850 10 35 10 19 23 29 9 | 68 43 57 74 64 80 63
XR04E | 1570 18 31 17 --- 22 38 12 | 67 48 67 --- 71 78 64
R05E | 1005 19 28 18 14 24 23 9 | 80 52 71 70 68 57 66
R07E | 1300 16 43 19 18 11 23 9 | 151 131 151 150 154 144 147
R08E | 1537 9 35 17 15 22 56 11 | 108 97 111 104 116 116 105
R09 | 1999 29 14 9 16 18 46 10 | 39 33 34 35 26 35 28
R11 | 1793 16 26 16 7 17 16 7 | 20 20 25 20 32 29 21
R12 | 660 12 17 10 17 15 16 6 | 19 17 24 31 20 19 18
R13 | 1427 41 63 36 31 52 31 18 | 27 36 46 48 27 35 30
R14 | 1344 12 21 11 16 11 25 7 | 19 26 28 34 22 32 23
R15 | 1035 11 17 29 14 20 40 10 | 20 27 31 28 26 37 22
R17 | 963 16 34 12 9 18 22 8 | 80 57 72 77 81 68 73
R18 | 1514 9 25 24 10 24 29 9 | 80 72 93 80 91 71 81
R19 | 2469 23 92 60 30 36 61 21 | 118 93 99 117 102 112 100
R20 | 1128 35 87 42 46 53 35 21 | 90 90 63 98 81 73 74
R21 | 1575 16 27 11 15 17 28 8 | 108 100 104 110 110 104 105
R24 | 1036 18 44 14 13 19 22 9 | 66 57 65 63 65 61 62
XR25 |15971 --- --- --- --- --- 7 0 | --- --- --- --- --- --- 0
------+-----------------------------------------+-------------------------------------
RMS | 1475 22 45 28 21 28 34 |T 71 60 69 74 70 69 65
WRMS | 1475 20 37 21 14 21 31 |NE 59 51 57 63 58 55 53
MEDI | 1344 16 31 17 15 20 28 |MD 80 52 65 74 71 68 64
Table 3.2223.1 GPS week: 2223 Day: 1 MJD: 59806
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 1248 55 64 63 35 24 47 22 | 66 36 58 53 50 54 43
R02E | 3249 8 29 14 13 17 25 8 | 86 83 82 82 95 81 83
R03E | 1239 8 48 18 14 26 30 10 | 47 30 41 54 73 63 49
XR04E | 886 17 37 14 --- 33 32 13 | 44 30 48 --- 76 57 49
R05E | 1542 26 41 17 11 16 22 10 | 71 37 50 51 62 56 54
R07E | 1546 17 30 22 16 18 28 9 | 97 88 99 102 108 84 96
R08E | 1028 21 29 22 18 24 46 12 | 96 97 108 103 110 100 99
R09 | 2534 20 11 9 14 32 17 8 | 22 18 18 22 21 20 14
R11 | 1231 11 13 15 12 13 17 6 | 13 21 35 29 25 29 23
R12 | 718 17 18 13 15 11 15 6 | 22 21 28 30 18 29 21
R13 | 1272 27 20 25 32 45 43 15 | 22 33 33 29 27 46 21
R14 | 1172 10 11 13 12 9 15 5 | 15 12 23 18 17 22 13
R15 | 867 11 12 14 19 15 18 7 | 19 15 22 33 15 28 20
R17 | 840 18 26 17 10 14 20 7 | 58 55 49 46 58 51 51
R18 | 1153 14 28 32 15 20 27 10 | 66 69 70 64 72 45 63
R19 | 2105 35 74 45 48 30 29 19 | 82 86 72 82 78 80 75
R20 | 1279 28 95 47 63 72 32 25 | 57 85 74 78 58 56 61
R21 | 914 12 34 11 18 24 19 8 | 95 89 96 102 98 85 94
R24 | 914 13 45 13 16 17 11 8 | 51 47 51 55 53 54 51
XR25 |16453 --- --- --- --- --- 8 0 | --- --- --- --- --- --- 0
------+-----------------------------------------+-------------------------------------
RMS | 1517 23 41 27 25 28 28 |T 54 50 55 57 58 54 51
WRMS | 1517 19 34 20 16 23 25 |NE 45 45 48 49 45 46 42
MEDI | 1231 17 29 17 15 20 22 |MD 57 37 50 53 58 54 51
Table 3.2223.2 GPS week: 2223 Day: 2 MJD: 59807
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 1419 55 60 66 37 21 20 19 | 79 29 37 58 49 52 43
R02E | 3379 8 31 15 17 16 23 8 | 94 96 100 113 94 85 96
R03E | 2052 12 41 16 19 15 17 8 | 62 45 51 65 64 62 58
XR04E | 2851 13 35 12 --- 13 16 8 | 52 39 54 --- 61 48 51
R05E | 1705 18 58 20 14 16 18 10 | 67 30 57 67 71 67 61
R07E | 829 19 30 17 26 20 24 10 | 83 60 76 85 77 71 74
R08E | 1329 17 26 14 14 25 32 10 | 50 44 51 41 59 47 45
R09 | 1544 15 20 11 9 20 12 6 | 30 29 35 28 23 21 24
R11 | 1289 14 16 22 14 8 19 7 | 20 24 42 23 21 24 20
R12 | 682 10 14 18 9 19 14 6 | 20 20 34 23 20 20 19
R13 | 1050 26 11 38 25 28 22 12 | 25 25 34 32 31 29 24
R14 | 930 11 10 14 16 11 21 6 | 29 30 30 30 26 24 25
R15 | 806 10 15 16 15 10 17 6 | 20 23 22 26 19 24 18
R17 | 780 24 23 16 8 17 27 9 | 71 60 64 68 78 65 67
R18 | 873 14 15 25 24 17 15 8 | 84 73 76 78 88 77 78
R19 | 1204 50 83 45 29 16 22 18 | 99 80 82 84 65 79 78
R20 | 1192 40 90 51 68 33 20 22 | 67 75 59 96 84 63 65
R21 | 1234 15 39 21 12 18 28 10 | 79 76 81 76 98 100 85
R24 | 1550 9 59 14 18 29 20 11 | 45 44 42 41 70 50 46
XR25 |19577 --- --- --- --- --- 9 0 | --- --- --- --- --- --- 0
------+-----------------------------------------+-------------------------------------
RMS | 1458 24 43 28 25 20 21 |T 56 47 54 57 57 53 51
WRMS | 1458 23 35 20 17 17 20 |NE 51 45 49 51 51 48 45
MEDI | 1234 15 30 17 16 17 20 |MD 62 44 51 58 64 52 51
Table 3.2223.3 GPS week: 2223 Day: 3 MJD: 59808
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 1475 56 58 54 60 15 18 20 | 99 35 37 87 67 48 55
R02E | 1533 9 29 15 25 21 20 8 | 70 50 74 80 64 69 67
R03E | 1281 20 38 22 18 17 15 9 | 74 37 52 66 63 64 58
XR04E | 1946 17 32 18 --- 17 22 10 | 60 46 65 --- 63 58 57
R05E | 1363 23 41 20 20 15 20 10 | 74 41 57 69 66 57 59
R07E | 617 17 31 15 15 22 17 8 | 74 42 54 69 57 69 60
R08E | 1239 14 29 14 24 17 18 8 | 54 35 49 62 56 48 48
R09 | 1551 17 20 15 17 20 39 10 | 30 32 37 39 32 46 32
R11 | 1560 19 15 16 17 22 18 8 | 28 33 38 36 43 33 32
R12 | 1753 18 14 17 23 18 16 8 | 27 30 37 34 32 22 25
R13 | 1231 18 17 30 32 60 25 14 | 30 31 30 34 36 28 25
R14 | 1398 8 15 9 15 12 26 7 | 26 24 30 33 28 44 29
R15 | 1009 9 10 15 13 16 17 6 | 26 31 38 35 30 32 30
R17 | 895 18 28 13 16 13 22 8 | 56 42 51 49 53 53 49
R18 | 869 18 20 24 22 19 14 8 | 69 58 70 64 72 59 64
R19 | 1319 59 109 52 63 56 32 27 | 102 79 64 104 65 79 70
R20 | 1912 59 65 47 67 72 19 24 | 85 62 48 87 66 73 61
R21 | 1490 23 30 10 22 19 25 9 | 60 52 55 59 58 52 52
R24 | 2502 13 49 16 19 32 10 10 | 53 28 51 48 75 48 48
XR25 | ---- --- --- --- --- --- 7 0 | --- --- --- --- --- --- 0
------+-----------------------------------------+-------------------------------------
RMS | 1449 28 41 26 32 31 22 |T 57 41 49 58 54 51 48
WRMS | 1449 20 32 20 20 22 20 |NE 53 41 45 54 50 47 44
MEDI | 1398 18 29 16 20 19 18 |MD 60 37 51 59 58 52 52
Table 3.2223.4 GPS week: 2223 Day: 4 MJD: 59809
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 1253 65 65 44 49 28 21 20 | 86 40 32 67 45 35 43
R02E | 1887 8 33 15 22 20 17 8 | 80 76 81 92 81 81 81
R03E | 1495 22 36 20 13 12 10 8 | 76 50 51 61 68 62 61
XR04E | 1386 15 32 21 --- 23 13 10 | 66 42 62 --- 70 51 57
R05E | 2215 23 30 19 23 18 18 9 | 62 37 53 60 55 44 48
R07E | 610 14 37 18 20 17 17 9 | 78 53 79 79 75 81 74
R08E | 1384 17 27 9 22 24 12 8 | 64 54 62 62 66 55 58
R09 | 1511 16 24 14 11 30 14 8 | 27 39 33 33 21 36 27
R11 | 1666 16 14 29 12 18 17 8 | 20 22 35 21 35 12 19
R12 | 1757 14 13 20 16 22 22 8 | 18 17 36 27 12 30 18
R13 | 1242 31 35 37 35 42 15 14 | 30 42 32 29 18 20 18
R14 | 1497 8 11 8 15 17 14 6 | 24 35 31 27 25 26 25
R15 | 849 4 12 19 25 17 16 7 | 22 25 32 39 19 21 22
R17 | 590 15 33 11 20 18 15 8 | 86 78 82 87 97 85 85
R18 | 754 15 23 28 18 19 15 9 | 121 123 122 116 128 115 120
R19 | 1618 59 103 67 55 40 22 25 | 111 96 91 107 96 89 91
R20 | 1317 60 55 44 53 35 24 19 | 84 102 72 99 55 67 70
R21 | 1427 15 33 11 21 18 13 8 | 70 64 68 68 82 77 71
R24 | 686 17 41 14 21 21 15 9 | 54 36 53 58 65 48 51
XR25 |12827 --- --- --- --- --- 5 0 | --- --- --- --- --- --- 0
------+-----------------------------------------+-------------------------------------
RMS | 1394 29 41 28 28 25 17 |T 62 54 58 62 58 54 54
WRMS | 1394 29 34 22 19 22 17 |NE 57 55 55 59 53 50 50
MEDI | 1386 16 33 19 21 20 15 |MD 66 42 53 61 65 51 57
Table 3.2223.5 GPS week: 2223 Day: 5 MJD: 59810
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 1062 64 63 47 39 20 20 19 | 81 24 32 64 50 48 44
R02E | 1484 7 35 18 27 18 20 9 | 69 61 70 87 80 65 70
R03E | 1663 23 28 21 16 16 13 8 | 66 45 52 61 63 58 57
XR04E | 1625 12 27 11 --- 18 11 8 | 61 49 60 --- 60 56 55
R05E | 1472 18 31 17 14 16 11 7 | 46 37 50 50 50 46 44
R07E | 473 22 31 12 14 13 18 8 | 77 53 63 67 72 68 66
R08E | 1950 12 31 9 19 13 18 7 | 63 51 61 58 65 71 61
R09 | 1020 12 23 10 17 14 12 6 | 23 28 27 34 27 20 21
R11 | 2979 17 19 18 30 31 18 10 | 24 28 33 42 26 31 23
R12 | 1790 14 14 21 14 25 19 8 | 26 21 33 31 32 15 21
R13 | 2331 17 29 27 10 32 19 10 | 27 33 32 38 25 24 26
R14 | 1818 12 13 13 21 16 11 6 | 31 30 28 40 20 22 25
R15 | 824 7 16 18 10 13 19 6 | 27 31 28 26 25 26 25
R17 | 633 18 31 11 18 17 10 7 | 51 49 51 52 62 52 51
R18 | 702 24 27 21 18 29 21 10 | 86 92 90 92 90 84 87
R19 | 2756 64 99 49 67 21 17 23 | 75 84 52 70 58 50 53
R20 | 959 42 60 63 81 46 31 24 | 73 50 52 89 58 65 58
R21 | 1173 12 33 17 17 14 14 7 | 57 48 57 63 56 59 55
R24 | 1225 20 38 15 14 22 16 9 | 62 60 54 56 69 50 56
XR25 | 8782 --- --- --- --- --- 4 0 | --- --- --- --- --- --- 0
------+-----------------------------------------+-------------------------------------
RMS | 1618 28 40 27 31 22 18 |T 53 46 48 56 52 47 47
WRMS | 1618 20 32 19 18 18 17 |NE 49 44 43 53 46 42 41
MEDI | 1472 17 31 18 17 18 17 |MD 61 48 52 56 58 50 53
Table 3.2223.6 GPS week: 2223 Day: 6 MJD: 59811
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 600 46 75 60 34 23 28 20 | 110 25 31 93 79 62 64
R02E | 2382 12 35 16 14 22 30 10 | 84 72 80 92 91 95 85
R03E | 2813 17 32 16 15 23 16 8 | 83 50 62 77 76 67 69
XR04E | 1305 10 30 18 --- 23 29 11 | 84 61 82 --- 83 81 79
R05E | 1345 12 44 22 15 15 17 9 | 72 46 63 70 67 67 64
R07E | 689 16 32 13 11 14 13 7 | 89 59 78 82 79 79 78
R08E | 1595 6 31 12 13 13 16 6 | 73 58 72 76 78 79 73
R09 | 1111 13 15 8 15 24 20 7 | 27 25 27 35 20 37 25
R11 | 4284 27 17 41 16 22 22 11 | 26 24 48 37 25 27 25
R12 | 1830 20 21 17 12 20 21 8 | 26 25 25 25 23 22 20
R13 | 2215 14 19 19 19 50 28 12 | 30 36 26 32 33 25 25
R14 | 2375 9 13 11 13 20 19 6 | 27 31 30 23 20 24 22
R15 | 1037 9 22 11 13 13 13 6 | 24 32 36 30 23 23 25
R17 | 834 9 31 17 11 20 17 7 | 67 47 57 64 70 59 60
R18 | 888 20 26 21 11 19 14 8 | 54 60 74 65 59 69 61
R19 | 1826 53 113 49 65 44 26 25 | 84 62 47 82 57 57 52
R20 | 938 44 71 62 86 42 26 25 | 76 52 39 90 57 61 53
R21 | 660 13 27 13 13 19 20 7 | 81 66 72 80 80 88 78
R24 | 1418 15 39 14 20 22 13 9 | 74 59 64 73 77 66 67
XR25 |10363 --- --- --- --- --- 8 0 | --- --- --- --- --- --- 0
------+-----------------------------------------+-------------------------------------
RMS | 1848 24 44 29 30 26 21 |T 62 46 53 62 57 57 53
WRMS | 1848 17 34 23 14 22 20 |NE 54 41 44 56 47 47 44
MEDI | 1345 14 31 17 14 22 19 |MD 73 50 57 70 67 62 61
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